High velocity tensile behavior of structural materials is essential to design impact-resistant structure. In case of automotive body, especially of energy absorbing members such as front side members, dynamic behavior of thin plate plays a key role to eyaluate their energy absorbing ability. So far, dynamic tensile mechanical properties of thin plate have not attracted impact researchers' and engineers' attention very much, exceptfor laminated composite materials. In this paper, with the one bar method that is known as an effective high velocity tensile testing technique for cylindrical specimen of various solid materials, the previous thin plate spccimen assembly was improved for steels and aluminum alloys. The most important factor is fastening technique between an impact block and the assembly. Because, we fOrmerly fastened them with a pin in order to allow slight misalignment of the assembly of the previous design. This pin fastening introduced a tremendous initial peak on stress-strain curves, even for aluminum alloys. A new assembly fastened by a screw solves this problem drastically. Stress-strain curves obtained by the one bar method, with the new specimen assembly, are almost equivalent to those obtained by the tensile version of the split Hopkinson pressure bar method.
View full abstract